Mechanisms and models of solid-propellant burn rate temperature sensitivity - A review
- 1 October 1985
- journal article
- review article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 23 (10), 1538-1547
- https://doi.org/10.2514/3.9121
Abstract
No abstract availableThis publication has 22 references indexed in Scilit:
- Model for double-base propellant combustionAIAA Journal, 1980
- Temperature Sensitivity of the Burning Rate of Composite Solid PropellantsCombustion Science and Technology, 1974
- Dynamic Responses of Solid Rockets during Rapid Pressure ChangeJournal of Spacecraft and Rockets, 1973
- The combustion of solid monopropellants and composite propellantsSymposium (International) on Combustion, 1971
- An Analysis of a Simplified Laminar Flame Theory for Solid Propellant CombustionCombustion Science and Technology, 1971
- Burning rate temperature sensitivity of composite solid propellantsJournal of Spacecraft and Rockets, 1971
- Theory of dynamic extinguishment of solid propellants with special reference to nonsteady heat feedback lawJournal of Spacecraft and Rockets, 1971
- A model of composite solid-propellant combustion based on multiple flamesAIAA Journal, 1970
- Initial temperature and pressure effects on composite solid-propellant burning rates - Comparisons with theoryAIAA Journal, 1970
- Temperature sensitivity of solid propellant burning rate.AIAA Journal, 1967